• 제목/요약/키워드: Frame Assembly

검색결과 159건 처리시간 0.022초

Seismic retrofit of framed structures using a steel frame assembly

  • Michael Adane;Seungho Chun;Jinkoo Kim
    • Steel and Composite Structures
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    • 제46권6호
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    • pp.857-865
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    • 2023
  • This study aimed to develop a seismic retrofit technique using a steel frame which can be easily transported and assembled on site. This enables the retrofit steel frame to be easily attached to an existing structure minimizing the unwanted gap between the structure and the steel frame assembly. A one-story one-bay RC frame was tested with and without seismic retrofit using the proposed steel frame to verify the seismic retrofit effect of the proposed system, and an analysis model was developed in Opensees for seismic performance evaluation of a case study soft first-story model structure retrofitted with the developed steel frame assembly. Seismic performance of the model structure was also evaluated considering soil structure interaction effect. The experimental study confirmed that the proposed seismic retrofit system can be applied effectively to improve the seismic performance of framed structures. Time history analysis results of the model structure showed that the proposed steel frame assembly was effective in increasing the seismic load resisting capacity of the soft first-story structure. However more steel frame assemblies were required to satisfy the given performance limit state of the model structure located on weak soil due to the negative soil-structure interaction effect.

Optimum distribution of steel frame assembly for seismic retrofit of framed structures

  • Michael Adane;Seungho Chun;Jinkoo Kim
    • Steel and Composite Structures
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    • 제50권3호
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    • pp.337-345
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    • 2024
  • This research proposed a particle swarm optimization (PSO) based seismic retrofit design of moment frame structures using a steel frame assembly. Two full scale specimens of the steel frame assembly with different corner details were attached to one-story RC frames for seismic retrofit, and the lateral load resisting capacities of the retrofitted frames subjected to cyclic loads were compared with those of a bare RC frame. The open source software framework Opensees was used to develop an analytical model for validating the experimental results. The developed analytical model and the optimization scheme were applied to a case study structure for economic seismic retrofit design, and its seismic performance was assessed before and after the retrofit. The results show that the developed steel frame assembly was effective in increasing seismic load resisting capability of the structure, and the PSO algorithm could be applied as convenient optimization tool for seismic retrofit design of structures.

과학로케트 날개조립체의 구조강도시험 및 안전성 평가 (Structural Test and Safety Evaluation for Fin Assembly of Scientific Sound Rocket)

  • 허용학;김갑순;주진원
    • 대한기계학회논문집
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    • 제18권12호
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    • pp.3395-3403
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    • 1994
  • The structural test technique and equipment for strength test of astronautical structures, such as rocket, were presented in this paper. Structural strength tests of the fin assembly with fin and fin frame in the scientific sound rocket were performed with load levels of 100% limit load and 150% ultimate load of design lift force. Safety factors in each part of the fin assembly were calculated at these two load levels and the stiffnesses based on the measured deflection of fin assembly and strains on fin and fin frame were evaluated at these two load level. As the result of structural test, the fin assembly was estimated to be safe.

LCD 디스플레이 프레임 조립 공정 최적화 연구 (A Study for Optimizing LCD Display Frame Assembly Process)

  • 윤철호
    • 한국산학기술학회논문지
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    • 제11권10호
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    • pp.3654-3657
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    • 2010
  • 본 연구에서는 LCD 디스플레이 프레임의 제품 원가를 절감하기 위해 조립공정의 최적화에 대해 연구하였다. 첫째로 OTRS를 이용하여 조립공정의 효율성을 분석하였고, 둘째로 낮은 가격의 원자재 코일을 대상으로 정해진 신뢰성 기준에 합격할 수 있는 프레임을 생산할 수 있는지 평가하였다. 연구 결과, 프레임 조립공정은 자동화가 상당 수준 진척되었기 때문에 높은 생산성이 유지되고 있다는 것을 알 수 있었고, 동시에 정해진 기준에 합격할 수 있는 프레임을 확보할 수 있는 가능성이 제시되었다.

Collapse-resistant performance of a single-story frame assembly and multi-story sub-frame under an internal column-removal scenario

  • Zhong, Wei-hui;Tan, Zheng;Tian, Li-min;Meng, Bao;Zheng, Yu-hui;Daun, Shi-chao
    • Steel and Composite Structures
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    • 제41권5호
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    • pp.663-679
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    • 2021
  • To elucidate the differences in the collapse behavior between a single-story beam-column assembly and multi-story frame, two 1/3-scale two-bay composite frames, including a single-story composite beam-column assembly and a three-story composite sub-frame, were designed and quasi-statically tested. The load-displacement responses, failure modes, and internal force development of the two frames were analyzed and compared in detail. Furthermore, the resistance mechanisms of the two specimens were explored, and the respective contributions of different load-resisting mechanisms to the total resistances were quantitatively separated to gain deeper insights. The experimental tests indicated that Vierendeel action was present in the two-dimensional multi-story frames, which led to an uneven internal force distribution among the three stories. The collapse resistance of TSDWA-3S in the flexural stage was not significantly increased by the structural redundancy provided by the additional story, as compared to that of TSDWA-1S. Although the development of the load response was similar in the two specimens at flexural stage, the collapse mechanisms of the multi-story composite frame were much more complicated than those of the single-story beam-column assembly, and the combined action between stories was critical in determining the internal force redistribution and rebalancing of the remaining structure.

항공기체구조의 정밀조립 및 동시설계 기술 (Accurate Assembly and Concurrent Design of Airframe Structures)

  • 박문식
    • 대한기계학회논문집A
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    • 제24권4호
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    • pp.811-823
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    • 2000
  • In design and manufacturing airframe structures which are composed of a lot of sub-assemblies and large complex profile shapes it is difficult to reduce so called hardware variations. Accordingly cost increasing factors for manufacturing airframe parts are much more than other machine parts because of the variability of fabricated details and assemlies. To improve cost and quality, accurate assembly methods and DPD techniques are proposed in this paper which are based upon using CAD/CAM techniques, the concept of KC's and the coordinated datum and index throughout the design, tooling, manufacturing and inspection. The proposed methods are applied to produce fuselage frame assemblies and related engineering aspects are described regarding the design of parts and tools in the context of concurrent digital definition. First articles and consequent mass production of frame assemblies shows a great improvement of the process capability ratio from 0.7 by the past processes to 1.0 by the proposed methods in addition to the cost reduction due to the less number of tools, reduced total assembly times and the space compaction needed by massive inventory. The need to achieve better Cpk, however, and future studies to be investigated will be addressed briefly.

가중치를 고려한 자동차 서브프레임의 인증 알고리즘 구현 (Development of Registration Algorithm considering Coordinate Weights for Automobile Sub-Frame Assembly)

  • 이광일;양승한;이영문
    • 한국기계가공학회지
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    • 제3권4호
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    • pp.7-12
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    • 2004
  • Inspection and analysis are essential process to determine whether a completed product is in given specification or not. Analysis of products with very complicated shape is difficult to carry out direct comparison between inspected coordinate and designed coordinates. So process called as matching or registrations is needed to solve this problem. By defining error between two coordinates and minimizing the error, registration is done. Registration consists of translation, rotation and scale transformations. Error must be defined to express feature of inspected product. In this paper, registration algorithm is developed to determine pose of sub-frame at assembly with body of automobile by defining error between two coordinates considering geometric feature of sub-frame.

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페이로드 페어링 체결 프레임에 대한 구조시험 (Structural Test for Assembly Frame of Payload Fairing)

  • 이종웅;장영순;이영무;공철원
    • 한국항공우주학회지
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    • 제35권12호
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    • pp.1129-1134
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    • 2007
  • 페이로드 페어링은 외부환경으로부터 위성 및 전자 탑재물들을 보호한다. 그리고 위성 분리 전에 페이로드 페어링은 투하 된다. 페어링 분리를 위하여 전단볼트로 체결된 체결프레임이 페이로드 페어링에 조립되어 있다. 전단볼트의 역할은 전체 구조하중을 견디며, 화약폭발력에 의해 절단이 된다. 그리고 전단볼트가 절단된 후 전단볼트로 연결되었던 체결 프레임은 분리된다. 본 논문에서는 전단볼트 설계에 대한 구조시험과 해석을 수행하였다. 구조시험은 체결 프레임을 포함한 하드웨어에 압축, 굽힘, 전단하중을 부가하였다. 시험결과 전단볼트는 비행하중 지지를 위한 구조강도와 화약폭발에 의해 절단되는데 요구되는 낮은 강도 조건을 만족하였다.

용접에 의한 자동차용 Frame의 변형과 잔류 응력 분석 (Deformation and Residual Stress of Automotive Frame by Welding)

  • 박태원;김기주;한창평;이영숙;임종한
    • 한국자동차공학회논문집
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    • 제19권5호
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    • pp.113-117
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    • 2011
  • The frame for automotive assembly can be deformed and remained on the residual stress due to high temperature thermal attacks when in welding. The frame deformation can be made to problems when in assembly with body and the residual stress can affect the negative effect on durability performance of the automobile. In order to analyze the frame deformation, the simplified test frame which had the similar shape (form) of the real automotive frame was fabricated. The contactless optical 3D scanner was used for the shape difference measurement of the frame between before and after the welding. The FE-model of the test frame was composed and the heat transfer and thermal stress simulation were performed. The simulated results were compared with the measured results for the reference of the frame design. The deformation shape of the frame by simulation was in good agreement with that by the experimental measurement.

그라운드 빔 조인트 기반 위상최적화법을 이용한 프레임 구조물의 조립 위치 및 강도 설정 (Ground Beam-Joint Topology Optimization for Design and Assembly of Multi-Piece Frame Structures)

  • 장강원;김명진;김윤영
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2007년도 춘계학술대회A
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    • pp.688-693
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    • 2007
  • Most frame structures cannot be manufactured in a single-piece form. Ideally, when a structure is built up by assembling multi pieces, assembly at the joints should be rigidly performed enough to have almost full stiffness, which is difficult for practical reasons such as manufacturing cost and time. In this research, we aim to develop a manufacturability-oriented compliance-minimizing topology optimization using a ground beam model incorporating additional zero-length elastic joint elements. In the present formulation, design variables control the stiffness of zero-length elastic joints, not the stiffness of beams. Because joint stiffness values at the converged state can be utilized to select candidate assembly locations and their strengths, the technique is extremely useful to design multi-piece frame structures. An optimal layout is also extracted based on the stiffness values.

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